Effect of hydrogen addition on the laminar burning velocity of n-decane/air mixtures: Experimental and numerical study

Hydrogen is a potential aviation alternative fuel. To explore the influence of hydrogen addition on the combustion of aviation kerosene, the spherical expanding flame method was used to measure the laminar burning velocity and Markstein length of n-decane/ hydrogen/air mixtures at 1bar, 2bar and 470 K using experimental and numerical analysis. The experimental LBVs agreed well with the simulation at an initial pressure of 1 bar, but lower than the simulation at 2bar. The laminar burning velocity showed a linear relationship with the hydrogen addition ratio (RH) at the different effective fuel-air equivalence ratios (fF). The Markstein length decreased with increased RH and initial pressure, hence, increasing the susceptibility of flame front instability. Based on a one-step overall reaction assumption, sensitivity analysis of the premixture mechanism showed that the kinetic effect greatly influenced n-decane/hydrogen/air mixture combustion. Further kinetic analysis indicated that the maximum (H + OH) mole fraction of the chemical reaction is highly responsible for the linear relationship between laminar burning velocity and RH. (c) 2022 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.

Automated summary

This study investigated the influence of hydrogen addition on the combustion of aviation kerosene by measuring the laminar burning velocity and Markstein length of n-decane/hydrogen/air mixtures. The research found that the laminar burning velocity showed a linear relationship with the hydrogen addition ratio, and the decreased Markstein length increased the flame front instability.